Abstract
With the continuous development of advanced fuel and engine technology, the boundary between liquid and solid fuel is more and more blurred, so the development of new solid-liquid two-phase fuels has become a major opportunity and challenge. Herein, two kinds of nAl@MOF energetic particles (nAl@Zn-MOF and nAl@Co-MOF) were fabricated by an in-situ electrostatic self-assembly method. The thermal property, ignition and combustion performances of nAl@MOF are characterized by TG-DSC, CO2 laser ignition and constant-volume combustion experiments. The results show that the initial exothermic temperature of nAl@Zn-MOF and nAl@Co-MOF are reduced by about 60 and 110 °C, respectively, compared with nAl (579.6 °C). Moreover, nAl@MOF has a lower ignition delay time, higher peak pressure, and faster pressurization rate than nAl, especially nAl@Zn-MOF-1 and nAl@Co-MOF-1. The combustion process of nAl@MOF is proposed, which can be obviously enhanced by regulating the interfacial reaction and the generation of microexplosions. In the ignition experiment of nanofluid fuel, nAl@MOF energetic particles exhibit the bifunction characteristics, which can simultaneously improve the ignition and combustion performances of solid-phase nAl particles and liquid-phase hydrocarbon fuel. This work provides a new strategy for advanced aerospace fuel by introducing MOF shells to construct bifunctional energetic particles with enhanced ignition and combustion properties.
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